View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 24936U 26145.31294808 +.00000000 +00000-0 +00000-0 0 00000
2 24936 8.0920 64.3488 0003081 1.0184 218.1718 1.00270575 09
| Epoch (UTC): | 25 May 2026 07:30:38 |
| Eccentricity: | 0.0003081 |
| inclination: | 8.0920° |
| perigee height: | 35774 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 64.3488° |
| argument of perigee: | 1.0184° |
| revolutions per day: | 1.00270575 |
| mean anomaly at epoch: | 218.1718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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